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S17400 Stainless Steel vs. 5040 Aluminum

S17400 stainless steel belongs to the iron alloys classification, while 5040 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is S17400 stainless steel and the bottom bar is 5040 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 280 to 440
66 to 74
Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 11 to 21
5.7 to 6.8
Fatigue Strength, MPa 380 to 670
100 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 570 to 830
140 to 150
Tensile Strength: Ultimate (UTS), MPa 910 to 1390
240 to 260
Tensile Strength: Yield (Proof), MPa 580 to 1250
190 to 230

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 850
190
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1400
600
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 17
160
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
41
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
130

Otherwise Unclassified Properties

Base Metal Price, % relative 14
9.5
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 2.7
8.3
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 160
14 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4060
260 to 380
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 32 to 49
24 to 26
Strength to Weight: Bending, points 27 to 35
31 to 32
Thermal Diffusivity, mm2/s 4.5
64
Thermal Shock Resistance, points 30 to 46
10 to 11

Alloy Composition

Aluminum (Al), % 0
95.2 to 98
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0.1 to 0.3
Copper (Cu), % 3.0 to 5.0
0 to 0.25
Iron (Fe), % 70.4 to 78.9
0 to 0.7
Magnesium (Mg), % 0
1.0 to 1.5
Manganese (Mn), % 0 to 1.0
0.9 to 1.4
Nickel (Ni), % 3.0 to 5.0
0
Niobium (Nb), % 0.15 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.3
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15